About: Issledovanie vliyaniya struktury i krivizny kompozicionnoho materiala na ustojchivost izolirovannoj kletki obshivki paneli nesuschej poverchnosti

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About: Issledovanie vliyaniya struktury i krivizny kompozicionnoho materiala na ustojchivost izolirovannoj kletki obshivki paneli nesuschej poverchnosti Goto Sponge NotDistinct Permalink

An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

Attributes	Values
rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	This project investigated: the effect of 90 ° layers on the stability of the wing skin isolated cells with simply supported edges of interregional passenger plane; the influence of the layers order with different reinforcement directions in the laminat on the critical buckling stress of the cells; the effect of curvature, which is characteristic for between-longeron and the bow parts of the upper wing skin, the stability of isolated cells with simply supported edges. Defined the influence of the structure of composite panels on its stability under pure compression with simple support edge and the optimal structure. Were estimated the curvature effect on stability of the composite panels. Were made recommendations about choosing the structure of composite material skin panels of the plane bearing surface (en) V dannom proekte issledovano: vlijanie sloev 90°na ustojchivost izolirovannoj kletki obshivki kryla megregionalnoho passagirskoho samoleta s scharnirno opertymi kromkami; vlijanie porjadka raspologeniya slojev s razlichnymi napravlenijami armirovaniya v pakete na kriticheskie naprjageniya poteri ustojchivosti kletki; vlijanie krivizny, harakternoj dla meglongeronnoj i nosovoj chastej verhnej obschivki kryla na ustojchivost izolirovannyh kletok s scharnirno opertymi kromkami. Provedeny ocenka vlijaniya struktury kompozicionnoj paneli na ustojchivost při sgatii i scharnirnom opiranii kromok i opredelenie optimalnoj struktury, a tak ge paschetnayz ocenka vlijaniya krivizny kompozicionnoj paneli na ustojchivost. Sformulirovany rekomendacii po vybor struktury panelej obschivki nesuschej poverhnosti samoleta iz KM
Title	Issledovanie vliyaniya struktury i krivizny kompozicionnoho materiala na ustojchivost izolirovannoj kletki obshivki paneli nesuschej poverchnosti Investigation of structure and curvature effects on the buckling stability of the bearing surface isolated cells of the composite material (en)
skos:prefLabel	Issledovanie vliyaniya struktury i krivizny kompozicionnoho materiala na ustojchivost izolirovannoj kletki obshivki paneli nesuschej poverchnosti Investigation of structure and curvature effects on the buckling stability of the bearing surface isolated cells of the composite material (en)
skos:notation	RIV/68407700:21220/12:00194726!RIV13-MSM-21220___
http://linked.open...avai/riv/aktivita	S
http://linked.open...avai/riv/aktivity	S
http://linked.open...vai/riv/dodaniDat	2013
http://linked.open...aciTvurceVysledku	Konovalova, Olga
http://linked.open.../riv/druhVysledku	O - Ostatní výsledky nezařaditelné do žádného z výše uvedených druhů výsledku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	České vysoké učení technické v Praze / Fakulta strojní
http://linked.open...dnocenehoVysledku	143147
http://linked.open...ai/riv/idVysledku	RIV/68407700:21220/12:00194726
http://linked.open...riv/jazykVysledku	rus - ruština
http://linked.open.../riv/klicovaSlova	buckling stability; laminate; layer; curvature; eigenvalue (en)
http://linked.open.../riv/klicoveSlovo	buckling stability curvature eigenvalue laminate layer
http://linked.open...ontrolniKodProRIV	[D686538BFA47]
http://linked.open...in/vavai/riv/obor	JI
http://linked.open...ichTvurcuVysledku	1 (xsd:int)
http://linked.open...cetTvurcuVysledku	1 (xsd:int)
http://linked.open...UplatneniVysledku	2012
http://linked.open...iv/tvurceVysledku	Konovalova, Olga
http://localhost/t...ganizacniJednotka	21220

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